View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 60943U 26145.58335647 +.00000000 +00000-0 -66902-3 0 00001
2 60943 53.1579 132.6613 0002066 69.2619 210.1769 15.34403372 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002066 |
| inclination: | 53.1579° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.6613° |
| argument of perigee: | 69.2619° |
| revolutions per day: | 15.34403372 |
| mean anomaly at epoch: | 210.1769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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